[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 8th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
163/14:26:51
484 -9
1 9
5 9
5
N/A 1
4 -0
0 192
1
000/00:33:42
967 -2
3 -0
3 190
4
163/18:35:11
563 3
7 8
5 8
5
N/A 5
2 -0
5 201
7
000/00:40:23
126 -5
6 0
4 193
2
166/15:04:46
859 8
7 9
8 9
8
N/A -4
1 0
3 205
3
000/00:29:33
717 2
1 0
6 196
2
166/19:08:06
571 -8
6 9
4 9
4
N/A -1
2 0
2 206
5
000/00:36:13
143 3
6 -0
3 205
3
Coasting Arc #1 (Orbit 3922)
---------------------------------------
Vector Time (GMT): 2011/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4131623
75 A = 6729289
84 meter
Y = 4870698
93 meter E =
0005333
Z = -2112808
96 I = 51
46056
XDOT = -5030
734529 Wp = 145
32333
YDOT = 1879
478516 meter/sec RA = 214
41552 deg
ZDOT = -5515
989417 TA = 58
34985
MA = 58
29785
Ha = 189
171 n
mi
Hp = 183
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13555196
01 X = 4087115
15
Y = 15979983
37 feet Y = 4916652
67 meter
Z = -6931787
93 Z = -2092845
15
XDOT = -16505
034544 XDOT = -5024
581827
YDOT = 6166
268098 feet/sec YDOT = 1823
256902 meter/sec
ZDOT = -18097
078141 ZDOT = -5540
413376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19143635
83 X = 5834980
20
Y = -8587004
17 feet Y = -2617318
87 meter
Z = -6851091
74 Z = -2088212
76
XDOT = 709
553858 XDOT = 216
272016
YDOT = 16070
038199 feet/sec YDOT = 4898
147643 meter/sec
ZDOT = -18196
083215 ZDOT = -5546
166164
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11157
52765734
00016717 00000-0 10270-3 0 9001
2 25544 51
6438 215
2651 0001291 294
6305 65
4724 15
74346790 39234
Satellite: ISS
Catalog Number: 25544
Epoch time: 11157
52765734 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 215
2651 deg
Eccentricity:
0001291
Arg of perigee: 294
6305 deg
Mean anomaly: 65
4724 deg
Mean motion: 15
74346790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3923
Checksum: 309
Coasting Arc #2 (Orbit 3938)
---------------------------------------
Vector Time (GMT): 2011/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4347130
66 A = 6721043
46 meter
Y = -1908110
76 meter E =
0006631
Z = 4754926
02 I = 51
45968
XDOT = 5087
012409 Wp = 49
49911
YDOT = 5185
662234 meter/sec RA = 209
22569 deg
ZDOT = -2563
197120 TA = 65
71238
MA = 65
64313
Ha = 188
902 n
mi
Hp = 183
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14262239
68 X = 4345046
00
Y = -6260205
92 feet Y = -1859510
68 meter
Z = 15600150
98 Z = 4776038
98
XDOT = 16689
673257 XDOT = 5041
098729
YDOT = 17013
327539 feet/sec YDOT = 5242
291858 meter/sec
ZDOT = -8409
439369 ZDOT = -2538
595518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2312646
27 X = -704894
58
Y = -15315849
38 feet Y = -4668270
89 meter
Z = 15685751
32 Z = 4781017
00
XDOT = 19699
861675 XDOT = 6004
517838
YDOT = -11507
249943 feet/sec YDOT = -3507
409783 meter/sec
ZDOT = -8309
951488 ZDOT = -2532
873214
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11158
54325384
00016717 00000-0 10270-3 0 9018
2 25544 51
6438 210
0472 0001479 299
0761 61
0254 15
74413301 39391
Satellite: ISS
Catalog Number: 25544
Epoch time: 11158
54325384 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 210
0472 deg
Eccentricity:
0001479
Arg of perigee: 299
0761 deg
Mean anomaly: 61
0254 deg
Mean motion: 15
74413301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3939
Checksum: 293
Coasting Arc #3 (Orbit 3954)
---------------------------------------
Vector Time (GMT): 2011/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4708032
95 A = 6728665
68 meter
Y = -4171842
74 meter E =
0013416
Z = 2369556
00 I = 51
51210
XDOT = 4920
912139 Wp = 68
77306
YDOT = -2485
379574 meter/sec RA = 204
11675 deg
ZDOT = 5381
916115 TA = 317
99336
MA = 318
09617
Ha = 189
230 n
mi
Hp = 183
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15446302
32 X = -4672543
52
Y = -13687148
10 feet Y = -4224292
62 meter
Z = 7774133
86 Z = 2346770
26
XDOT = 16144
724867 XDOT = 4922
194103
YDOT = -8154
132459 feet/sec YDOT = -2430
344278 meter/sec
ZDOT = 17657
205102 ZDOT = 5405
824718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17081901
91 X = -5206563
70
Y = 11643007
33 feet Y = 3548788
63 meter
Z = 7681955
69 Z = 2341460
09
XDOT = -3101
436930 XDOT = -945
317976
YDOT = -16307
221639 feet/sec YDOT = -4970
441156 meter/sec
ZDOT = 17754
157768 ZDOT = 5411
467288
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11159
55882828
00016717 00000-0 10270-3 0 9022
2 25544 51
6435 204
8285 0001292 315
8510 44
2550 15
74397162 39559
Satellite: ISS
Catalog Number: 25544
Epoch time: 11159
55882828 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 204
8285 deg
Eccentricity:
0001292
Arg of perigee: 315
8510 deg
Mean anomaly: 44
2550 deg
Mean motion: 15
74397162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3955
Checksum: 315
Coasting Arc #4 (Orbit 3969)
---------------------------------------
Vector Time (GMT): 2011/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4241930
85 A = 6721505
69 meter
Y = 2429795
31 meter E =
0009599
Z = -4622276
10 I = 51
51826
XDOT = -5642
066707 Wp = 106
02897
YDOT = -4361
211291 meter/sec RA = 198
92648 deg
ZDOT = 2887
595327 TA = 192
60920
MA = 192
63323
Ha = 189
092 n
mi
Hp = 183
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13917095
97 X = -4246331
81
Y = 7971769
39 feet Y = 2382335
26 meter
Z = -15164947
82 Z = -4642893
90
XDOT = -18510
717542 XDOT = -5606
906902
YDOT = -14308
435994 feet/sec YDOT = -4424
107976 meter/sec
ZDOT = 9473
737951 ZDOT = 2860
271147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4582606
67 X = 1396778
51
Y = 15286958
30 feet Y = 4659464
89 meter
Z = -15248571
47 Z = -4647764
58
XDOT = -17075
088478 XDOT = -5204
486968
YDOT = 14450
649599 feet/sec YDOT = 4404
557998 meter/sec
ZDOT = 9363
167246 ZDOT = 2853
893377
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11160
51090269
00016717 00000-0 10270-3 0 9031
2 25544 51
6444 199
9362 0001396 317
8134 42
2921 15
74451614 39708
Satellite: ISS
Catalog Number: 25544
Epoch time: 11160
51090269 = yrday
fracday
Element set: 903
Inclination: 51
6444 deg
RA of node: 199
9362 deg
Eccentricity:
0001396
Arg of perigee: 317
8134 deg
Mean anomaly: 42
2921 deg
Mean motion: 15
74451614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3970
Checksum: 303
Coasting Arc #5 (Orbit 3985)
---------------------------------------
Vector Time (GMT): 2011/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5106164
20 A = 6727641
93 meter
Y = 3456054
04 meter E =
0003687
Z = -2691666
27 I = 51
56909
XDOT = -4798
070959 Wp = 118
76187
YDOT = 3056
182556 meter/sec RA = 193
82524 deg
ZDOT = -5185
073491 TA = 91
95069
MA = 91
90846
Ha = 189
095 n
mi
Hp = 183
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16752507
22 X = 5080214
14
Y = 11338759
97 feet Y = 3513009
44 meter
Z = -8830926
10 Z = -2666923
08
XDOT = -15741
702621 XDOT = -4806
700882
YDOT = 10026
845657 feet/sec YDOT = 3002
479866 meter/sec
ZDOT = -17011
395967 ZDOT = -5208
403318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14656126
92 X = 4467187
49
Y = -14006096
48 feet Y = -4269058
21 meter
Z = -8730775
26 Z = -2661140
30
XDOT = 5445
340327 XDOT = 1659
739732
YDOT = 16346
537329 feet/sec YDOT = 4982
424578 meter/sec
ZDOT = -17106
037611 ZDOT = -5213
920264
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11161
52642452
00016717 00000-0 10270-3 0 9041
2 25544 51
6447 194
7177 0001348 324
0101 36
0971 15
74510124 39864
Satellite: ISS
Catalog Number: 25544
Epoch time: 11161
52642452 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 194
7177 deg
Eccentricity:
0001348
Arg of perigee: 324
0101 deg
Mean anomaly: 36
0971 deg
Mean motion: 15
74510124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3986
Checksum: 289
Coasting Arc #6 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2011/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4128522
46 A = 6721943
58 meter
Y = -2921771
86 meter E =
0008988
Z = 4423395
07 I = 51
57950
XDOT = 6013
804549 Wp = 59
61780
YDOT = 3535
353106 meter/sec RA = 188
63517 deg
ZDOT = -3268
330701 TA = 63
21454
MA = 63
12262
Ha = 188
937 n
mi
Hp = 183
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13545021
19 X = 4139399
18
Y = -9585865
68 feet Y = -2875543
93 meter
Z = 14512451
01 Z = 4443477
68
XDOT = 19730
329886 XDOT = 5989
701688
YDOT = 11598
927513 feet/sec YDOT = 3602
468745 meter/sec
ZDOT = -10722
869755 ZDOT = -3239
173497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6760704
93 X = -2060662
86
Y = -15075724
61 feet Y = -4595080
86 meter
Z = 14593938
82 Z = 4448232
55
XDOT = 14154
755458 XDOT = 4314
369464
YDOT = -16643
256767 feet/sec YDOT = -5072
864663 meter/sec
ZDOT = -10604
825700 ZDOT = -3232
350873
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11162
54191985
00016717 00000-0 10270-3 0 9055
2 25544 51
6434 189
4992 0001416 329
7045 30
4037 15
74567225 40026
Satellite: ISS
Catalog Number: 25544
Epoch time: 11162
54191985 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 189
4992 deg
Eccentricity:
0001416
Arg of perigee: 329
7045 deg
Mean anomaly: 30
4037 deg
Mean motion: 15
74567225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4002
Checksum: 305
Coasting Arc #7 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2011/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905423
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5351516
90 A = 6726693
55 meter
Y = -2724499
86 meter E =
0013008
Z = 3016638
48 I = 51
62537
XDOT = 4651
058837 Wp = 77
54346
YDOT = -3638
930606 meter/sec RA = 183
54089 deg
ZDOT = 4949
347757 TA = 317
38717
MA = 317
48802
Ha = 189
184 n
mi
Hp = 183
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17557470
13 X = -5335307
70
Y = -8938647
84 feet Y = -2784253
59 meter
Z = 9897107
88 Z = 2990679
52
XDOT = 15259
379387 XDOT = 4667
361104
YDOT = -11938
748707 feet/sec YDOT = -3586
829216 meter/sec
ZDOT = 16238
017575 ZDOT = 4971
981896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11949704
21 X = -3642269
84
Y = 15730176
64 feet Y = 4794557
84 meter
Z = 9791988
53 Z = 2984598
10
XDOT = -7881
412556 XDOT = -2402
254547
YDOT = -16183
734200 feet/sec YDOT = -4932
802184 meter/sec
ZDOT = 16329
883639 ZDOT = 4977
348533
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11163
55739118
00016717 00000-0 10270-3 0 9064
2 25544 51
6429 184
2801 0001431 339
3731 20
7375 15
74565227 40182
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
55739118 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 184
2801 deg
Eccentricity:
0001431
Arg of perigee: 339
3731 deg
Mean anomaly: 20
7375 deg
Mean motion: 15
74565227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4018
Checksum: 300
Coasting Arc #8 (Orbit 4018)
---------------------------------------
Vector Time (GMT): 2011/163/14:43:42
967
Vector Time (MET): N/A
Weight (LBS) : 903960
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5273680
32 A = 6734186
02 meter
Y = 2432836
09 meter E =
0005754
Z = -3405705
16 I = 51
62312
XDOT = -4777
175119 Wp = 252
36858
YDOT = -3895
389639 meter/sec RA = 182
90624 deg
ZDOT = 4606
660338 TA = 67
44646
MA = 67
38558
Ha = 192
137 n
mi
Hp = 190
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17302100
78 X = -5283948
34
Y = 7981745
71 feet Y = 2373805
69 meter
Z = -11173573
35 Z = -3431349
53
XDOT = -15673
146716 XDOT = -4755
639612
YDOT = -12780
149735 feet/sec YDOT = -3948
691192 meter/sec
ZDOT = 15113
715020 ZDOT = 4583
504312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15665539
58 X = 4774856
46
Y = 10739008
73 feet Y = 3273249
86 meter
Z = -11277599
85 Z = -3437412
43
XDOT = -2150
198267 XDOT = -655
380432
YDOT = 18937
481564 feet/sec YDOT = 5772
144381 meter/sec
ZDOT = 15019
996344 ZDOT = 4578
094886
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11163
62087358
00016717 00000-0 10270-3 0 9075
2 25544 51
6411 183
9539 0010580 261
4051 98
5912 15
71496982 40191
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
62087358 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 183
9539 deg
Eccentricity:
0010580
Arg of perigee: 261
4051 deg
Mean anomaly: 98
5912 deg
Mean motion: 15
71496982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4019
Checksum: 320
Coasting Arc #9 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2011/163/18:55:23
126
Vector Time (MET): N/A
Weight (LBS) : 902208
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4293872
34 A = 6742844
62 meter
Y = 3320509
82 meter E =
0009056
Z = -3995089
76 I = 51
62444
XDOT = -5921
183207 Wp = 169
82329
YDOT = 2916
599100 meter/sec RA = 182
06417 deg
ZDOT = -3949
988476 TA = 59
30016
MA = 59
21096
Ha = 201
654 n
mi
Hp = 193
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14087507
69 X = 4275830
24
Y = 10894061
08 feet Y = 3368426
24 meter
Z = -13107249
85 Z = -3974273
23
XDOT = -19426
454090 XDOT = -5934
168583
YDOT = 9568
894686 feet/sec YDOT = 2850
312839 meter/sec
ZDOT = -12959
279777 ZDOT = -3978
784963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14858450
17 X = -4528855
61
Y = -9928069
84 feet Y = -3026075
69 meter
Z = -13022992
21 Z = -3969408
03
XDOT = 17945
815193 XDOT = 5469
884471
YDOT = -9749
260800 feet/sec YDOT = -2971
574692 meter/sec
ZDOT = -13076
102299 ZDOT = -3985
595981
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11163
81174145
00016717 00000-0 10270-3 0 9088
2 25544 51
6430 182
9790 0012067 204
3003 155
7589 15
67878273 40227
Satellite: ISS
Catalog Number: 25544
Epoch time: 11163
81174145 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 182
9790 deg
Eccentricity:
0012067
Arg of perigee: 204
3003 deg
Mean anomaly: 155
7589 deg
Mean motion: 15
67878273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 309
Coasting Arc #10 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2011/164/18:55:23
126
Vector Time (MET): N/A
Weight (LBS) : 902208
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2863068
38 A = 6739948
50 meter
Y = -3881300
74 meter E =
0007072
Z = 4704037
27 I = 51
64492
XDOT = 6954
764909 Wp = 171
63452
YDOT = 1805
714112 meter/sec RA = 176
92957 deg
ZDOT = -2749
403949 TA = 305
44413
MA = 305
51013
Ha = 201
321 n
mi
Hp = 193
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9393268
95 X = 2883405
51
Y = -12733926
33 feet Y = -3849171
31 meter
Z = 15433193
16 Z = 4717994
87
XDOT = 22817
470175 XDOT = 6947
412374
YDOT = 5924
258896 feet/sec YDOT = 1883
445898 meter/sec
ZDOT = -9020
354163 ZDOT = -2715
634977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8203408
39 X = -2500398
88
Y = 13466121
89 feet Y = 4104473
95 meter
Z = 15489915
57 Z = 4721326
27
XDOT = -22304
406847 XDOT = -6798
383207
YDOT = -3392
839466 feet/sec YDOT = -1034
137469 meter/sec
ZDOT = -8883
526717 ZDOT = -2707
698943
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11164
83154208
00016717 00000-0 10270-3 0 9090
2 25544 51
6422 177
7899 0012050 208
4572 151
5931 15
67902520 40383
Satellite: ISS
Catalog Number: 25544
Epoch time: 11164
83154208 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 177
7899 deg
Eccentricity:
0012050
Arg of perigee: 208
4572 deg
Mean anomaly: 151
5931 deg
Mean motion: 15
67902520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 307
Coasting Arc #11 (Orbit 4053)
---------------------------------------
Vector Time (GMT): 2011/165/18:55:23
126
Vector Time (MET): N/A
Weight (LBS) : 902208
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6708622
89 A = 6749462
38 meter
Y = 563227
84 meter E =
0003949
Z = 495823
19 I = 51
70747
XDOT = 44
021549 Wp = 117
33299
YDOT = -4794
797399 meter/sec RA = 171
86736 deg
ZDOT = 6003
932422 TA = 248
03685
MA = 248
07883
Ha = 201
164 n
mi
Hp = 193
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22009917
63 X = -6716831
04
Y = 1847860
35 feet Y = 488161
95 meter
Z = 1626716
49 Z = 463212
76
XDOT = 144
427653 XDOT = 68
468523
YDOT = -15730
962594 feet/sec YDOT = -4794
169603 meter/sec
ZDOT = 19697
941018 ZDOT = 6004
204727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21721151
32 X = 6620606
92
Y = -4056523
94 feet Y = -1236428
50 meter
Z = 1494479
03 Z = 455517
21
XDOT = 1262
614550 XDOT = 384
844915
YDOT = 14068
699245 feet/sec YDOT = 4288
139530 meter/sec
ZDOT = 19699
223410 ZDOT = 6004
323295
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11165
85132535
00016717 00000-0 10270-3 0 9104
2 25544 51
6424 172
5993 0012029 212
4586 147
5836 15
67912339 40545
Satellite: ISS
Catalog Number: 25544
Epoch time: 11165
85132535 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 172
5993 deg
Eccentricity:
0012029
Arg of perigee: 212
4586 deg
Mean anomaly: 147
5836 deg
Mean motion: 15
67912339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4054
Checksum: 313
Coasting Arc #12 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2011/166/15:19:33
717
Vector Time (MET): N/A
Weight (LBS) : 900926
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3250959
83 A = 6749445
37 meter
Y = -4132477
98 meter E =
0012143
Z = 4219555
49 I = 51
70441
XDOT = 6613
906172 Wp = 107
61436
YDOT = 1480
172078 meter/sec RA = 167
51396 deg
ZDOT = -3641
087147 TA = 19
49481
MA = 19
44841
Ha = 205
253 n
mi
Hp = 196
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10665878
72 X = 3276430
58
Y = -13557998
63 feet Y = -4095982
21 meter
Z = 13843686
00 Z = 4235409
68
XDOT = 21699
167230 XDOT = 6614
550752
YDOT = 4856
207606 feet/sec YDOT = 1554
137127 meter/sec
ZDOT = -11945
823974 ZDOT = -3608
954971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17141055
87 X = -5224593
83
Y = 1405720
46 feet Y = 428463
60 meter
Z = 13908130
42 Z = 4239198
15
XDOT = -11080
493308 XDOT = -3377
334360
YDOT = -18049
582660 feet/sec YDOT = -5501
512795 meter/sec
ZDOT = -11815
584726 ZDOT = -3601
390225
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11166
67999227
00016717 00000-0 10270-3 0 9115
2 25544 51
6394 168
3818 0006773 162
7985 197
3404 15
65249713 40674
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
67999227 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 168
3818 deg
Eccentricity:
0006773
Arg of perigee: 162
7985 deg
Mean anomaly: 197
3404 deg
Mean motion: 15
65249713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 353
Coasting Arc #13 (Orbit 4069)
---------------------------------------
Vector Time (GMT): 2011/166/19:26:13
143
Vector Time (MET): N/A
Weight (LBS) : 899355
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6629987
03 A = 6766127
86 meter
Y = 619214
23 meter E =
0007782
Z = 1172145
05 I = 51
73573
XDOT = 583
885781 Wp = 33
96104
YDOT = -4905
406969 meter/sec RA = 166
68351 deg
ZDOT = 5881
564184 TA = 338
79492
MA = 338
82715
Ha = 206
511 n
mi
Hp = 205
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21751925
96 X = -6642112
50
Y = 2031542
74 feet Y = 545005
65 meter
Z = 3845620
25 Z = 1139907
32
XDOT = 1915
635763 XDOT = 610
124091
YDOT = -16093
854886 feet/sec YDOT = -4898
732078 meter/sec
ZDOT = 19296
470420 ZDOT = 5884
463443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20572823
45 X = 6270596
59
Y = -7417608
77 feet Y = -2260887
15 meter
Z = 3714870
08 Z = 1132292
40
XDOT = 1744
970585 XDOT = 531
867034
YDOT = 14530
887819 feet/sec YDOT = 4429
014607 meter/sec
ZDOT = 19308
412822 ZDOT = 5885
204228
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11166
87166464
00016717 00000-0 10270-3 0 9127
2 25544 51
6417 167
4130 0007321 262
9601 97
0723 15
61954699 40701
Satellite: ISS
Catalog Number: 25544
Epoch time: 11166
87166464 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 167
4130 deg
Eccentricity:
0007321
Arg of perigee: 262
9601 deg
Mean anomaly: 97
0723 deg
Mean motion: 15
61954699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4070
Checksum: 312
Coasting Arc #14 (Orbit 4084)
---------------------------------------
Vector Time (GMT): 2011/167/19:26:13
143
Vector Time (MET): N/A
Weight (LBS) : 899355
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4381553
06 A = 6757697
75 meter
Y = 2351996
64 meter E =
0003633
Z = -4578902
12 I = 51
73724
XDOT = -5530
951676 Wp = 33
37163
YDOT = 4366
338855 meter/sec RA = 161
65730 deg
ZDOT = -3047
936456 TA = 206
24781
MA = 206
26623
Ha = 206
204 n
mi
Hp = 205
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14375174
10 X = 4377170
24
Y = 7716524
42 feet Y = 2400970
22 meter
Z = -15022644
76 Z = -4557626
88
XDOT = -18146
166915 XDOT = -5564
559634
YDOT = 14325
258710 feet/sec YDOT = 4304
301080 meter/sec
ZDOT = -9999
791523 ZDOT = -3074
886398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15999845
01 X = -4876752
76
Y = -3574592
05 feet Y = -1089535
66 meter
Z = -14936448
25 Z = -4552629
43
XDOT = 13345
126428 XDOT = 4067
594535
YDOT = -17465
975139 feet/sec YDOT = -5323
629222 meter/sec
ZDOT = -10109
259706 ZDOT = -3081
302358
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11167
83134786
00016717 00000-0 10270-3 0 9137
2 25544 51
6420 162
5722 0007435 266
8566 93
1740 15
61990614 40856
Satellite: ISS
Catalog Number: 25544
Epoch time: 11167
83134786 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 162
5722 deg
Eccentricity:
0007435
Arg of perigee: 266
8566 deg
Mean anomaly: 93
1740 deg
Mean motion: 15
61990614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4085
Checksum: 317
Coasting Arc #15 (Orbit 4100)
---------------------------------------
Vector Time (GMT): 2011/168/19:26:13
143
Vector Time (MET): N/A
Weight (LBS) : 899355
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 171158
39 A = 6755346
93 meter
Y = -4444107
07 meter E =
0004470
Z = 5088414
86 I = 51
75881
XDOT = 7292
265741 Wp = 312
65323
YDOT = -1685
084976 meter/sec RA = 156
58480 deg
ZDOT = -1714
996561 TA = 153
87968
MA = 153
85712
Ha = 205
889 n
mi
Hp = 205
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 561543
29 X = 196122
22
Y = -14580403
78 feet Y = -4442054
43 meter
Z = 16694274
49 Z = 5089306
17
XDOT = 23924
756367 XDOT = 7318
897754
YDOT = -5528
494015 feet/sec YDOT = -1603
389210 meter/sec
ZDOT = -5626
629138 ZDOT = -1679
506752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3690525
45 X = 1124872
16
Y = 14112303
51 feet Y = 4301430
11 meter
Z = 16698060
29 Z = 5089568
78
XDOT = -20379
027710 XDOT = -6211
527646
YDOT = 11824
305736 feet/sec YDOT = 3604
048388 meter/sec
ZDOT = -5482
606916 ZDOT = -1671
098588
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11168
85499747
00016717 00000-0 10270-3 0 9142
2 25544 51
6424 157
4082 0007486 270
6399 89
3900 15
62036215 41018
Satellite: ISS
Catalog Number: 25544
Epoch time: 11168
85499747 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 157
4082 deg
Eccentricity:
0007486
Arg of perigee: 270
6399 deg
Mean anomaly: 89
3900 deg
Mean motion: 15
62036215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4101
Checksum: 324
Coasting Arc #16 (Orbit 4115)
---------------------------------------
Vector Time (GMT): 2011/169/19:26:13
143
Vector Time (MET): N/A
Weight (LBS) : 899355
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4429716
77 A = 6764035
07 meter
Y = 4522589
71 meter E =
0005623
Z = -2371801
86 I = 51
81503
XDOT = -5039
302976 Wp = 322
64875
YDOT = -2101
513628 meter/sec RA = 151
54324 deg
ZDOT = 5402
185140 TA = 10
84125
MA = 10
82914
Ha = 206
152 n
mi
Hp = 205
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14533191
51 X = -4468438
39
Y = 14837892
76 feet Y = 4472837
81 meter
Z = -7781502
17 Z = -2393414
45
XDOT = -16533
146246 XDOT = -5041
671393
YDOT = -6894
729750 feet/sec YDOT = -2157
880301 meter/sec
ZDOT = 17723
704526 ZDOT = 5377
698436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9369149
84 X = 2855716
87
Y = -18499210
42 feet Y = -5638559
34 meter
Z = -7869354
37 Z = -2398579
21
XDOT = 16591
907232 XDOT = 5057
213324
YDOT = 902
739789 feet/sec YDOT = 275
155088 meter/sec
ZDOT = 17624
446736 ZDOT = 5371
931365
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11169
81465861
00016717 00000-0 10270-3 0 9150
2 25544 51
6424 152
5667 0007521 274
7684 85
2614 15
62015086 41161
Satellite: ISS
Catalog Number: 25544
Epoch time: 11169
81465861 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 152
5667 deg
Eccentricity:
0007521
Arg of perigee: 274
7684 deg
Mean anomaly: 85
2614 deg
Mean motion: 15
62015086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4116
Checksum: 315
Coasting Arc #17 (Orbit 4131)
---------------------------------------
Vector Time (GMT): 2011/170/19:26:13
143
Vector Time (MET): N/A
Weight (LBS) : 899355
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6090613
13 A = 6765082
33 meter
Y = -2267416
72 meter E =
0005616
Z = -1865286
27 I = 51
84433
XDOT = 200
291516 Wp = 212
36606
YDOT = 5192
788633 meter/sec RA = 146
54858 deg
ZDOT = -5655
080282 TA = 348
17236
MA = 348
18554
Ha = 206
411 n
mi
Hp = 205
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19982326
53 X = 6124576
25
Y = -7439031
23 feet Y = -2199117
62 meter
Z = -6119705
60 Z = -1835616
30
XDOT = 657
124396 XDOT = 169
680844
YDOT = 17036
708114 feet/sec YDOT = 5194
858061 meter/sec
ZDOT = -18553
412999 ZDOT = -5654
180897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16638012
96 X = -5071266
35
Y = 13389137
78 feet Y = 4081009
20 meter
Z = -5999239
11 Z = -1828568
08
XDOT = -5140
983836 XDOT = -1566
971873
YDOT = -14704
884687 feet/sec YDOT = -4482
048853 meter/sec
ZDOT = -18549
963672 ZDOT = -5654
028927
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11170
83828388
00016717 00000-0 10270-3 0 9162
2 25544 51
6423 147
4033 0007570 277
1765 82
8531 15
62010203 41326
Satellite: ISS
Catalog Number: 25544
Epoch time: 11170
83828388 = yrday
fracday
Element set: 916
Inclination: 51
6423 deg
RA of node: 147
4033 deg
Eccentricity:
0007570
Arg of perigee: 277
1765 deg
Mean anomaly: 82
8531 deg
Mean motion: 15
62010203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4132
Checksum: 292
Coasting Arc #18 (Orbit 4147)
---------------------------------------
Vector Time (GMT): 2011/171/19:26:13
143
Vector Time (MET): N/A
Weight (LBS) : 899355
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4414453
58 A = 6756213
79 meter
Y = -1424090
59 meter E =
0002468
Z = 4914343
78 I = 51
83932
XDOT = 4437
847183 Wp = 219
06220
YDOT = -5831
764424 meter/sec RA = 141
51824 deg
ZDOT = 2295
236150 TA = 208
58961
MA = 208
60315
Ha = 206
921 n
mi
Hp = 205
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14483115
41 X = -4422073
73
Y = -4672213
22 feet Y = -1473498
90 meter
Z = 16123175
13 Z = 4892879
94
XDOT = 14559
866085 XDOT = 4491
579561
YDOT = -19133
085381 feet/sec YDOT = -5781
837565 meter/sec
ZDOT = 7530
302330 ZDOT = 2316
924753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15303363
47 X = 4664465
18
Y = -443106
38 feet Y = -135058
82 meter
Z = 16036137
56 Z = 4887814
73
XDOT = -7357
740748 XDOT = -2242
639380
YDOT = 21754
700690 feet/sec YDOT = 6630
832770 meter/sec
ZDOT = 7618
533082 ZDOT = 2322
128883
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 11171
86189578
00016717 00000-0 10270-3 0 9178
2 25544 51
6422 142
2385 0007442 282
5511 77
4814 15
62033687 41487
Satellite: ISS
Catalog Number: 25544
Epoch time: 11171
86189578 = yrday
fracday
Element set: 917
Inclination: 51
6422 deg
RA of node: 142
2385 deg
Eccentricity:
0007442
Arg of perigee: 282
5511 deg
Mean anomaly: 77
4814 deg
Mean motion: 15
62033687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4148
Checksum: 319
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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